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Comparison of aerodynamic performance of several STOL conceptsWind tunnel tests to determine the aerodynamic characteristics of basically similar short takeoff aircraft were conducted. The investigations were designed to provide data for a systematic direct comparison of five of the concepts considered. The configurations of the five models are illustrated and described. The aerodynamic data are presented in the form of graphs. It was concluded that the most complex systems require the least amount of net thrust.
Document ID
19730024211
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoad, D. R. (Army Air Mobility Research and Development Lab. Hampton, VA, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: NASA. Langley Res. Center STOL Technol.
Subject Category
Aircraft
Accession Number
73N32944
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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